Analysis of Low Speed Unsteady Airfoil Flows. Hsun Chen, Jian P. Shao, Kuo-cheng Chang, Max Platzer, Tuncer Cebeci

Analysis of Low Speed Unsteady Airfoil Flows



Download Analysis of Low Speed Unsteady Airfoil Flows



Analysis of Low Speed Unsteady Airfoil Flows Hsun Chen, Jian P. Shao, Kuo-cheng Chang, Max Platzer, Tuncer Cebeci ebook djvu
Publisher: Springer
Language: German
Page: 235
ISBN: 3540229329, 9783540229322

The authors take the view that a full understanding of the physics of lift generation is possible only by considering the unsteady aerodynamics of the starting vortex generation process. This view is also reflected in the methods of computational fluid dynamics when accurate steady-state solutions can be obtained by solving unsteady flow equations. This comprehensive textbook concentrates on unsteady low-speed flows over airfoils while restricting the discussions to two-dimensional incompressible flows. It first describes the physics of unsteady flow mechanisms for the generation of lift and of thrust on flapping wings and then the Navier-Stokes equations and their Reynolds-averaged form. The bulk of the book addresses three methods for the computation of steady and unsteady airfoil flows based on the so-called panel method pioneered by the senior author of this book. Many applications of practical importance in industry are considered, and the computer programs together with the accompanying CD-ROMs are carefully documented.

From the Back Cover

This book provides an introduction to unsteady aerodynamics with emphasis on the analysis and computation of inviscid and viscous two-dimensional flows over airfoils at low speeds. It begins with a discussion of the physics of unsteady flows and an explanation of lift and thrust generation, airfoil flutter, gust response and dynamic stall. This is followed by an exposition of the four major calculation methods in currents use, namely inviscid-panel, boundary-layer, viscous-inviscid interaction and Navier-Stokes methods. Examples are provided to demonstrate the use of each method and panel and interactive boundary layer codes are included on the CD-ROM. Undergraduate and graduate students, teachers, scientists and engineers concerned with aeronautical, hydronautical and mechanical engineering problems will gain understanding of the physics of unsteady low-speed flows and an ability to analyze these flows with modern computational methods.



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